Steel Structure
Q235/Q355 Grade Steel
H-Shaped Steel
C/Z Section Steel
Insulation Panel (EPS/PU/Rock Wool), Metal Sheet
Crane, Drainage Pipe, Door, Window
Over 25 Years
30 Days After Receiving the Deposit
T/T, L/C, PayPal
A steel aircraft hangar at this scale is not a scaled-up shed. It is a hybrid structure — rigid welded portal frames carrying vertical and lateral load down to the foundation, spanning a space-truss or space-grid roof that keeps every column out of the floor plate. That combination is what allows a 60 m to 180 m column-free clear span with clear heights from 15 m upward, while carrying 20 to 50 tonnes of crane load off the roof structure and taking the full thrust of a door wider than a tennis court.
Every frame is calculated for the site it will actually stand on: gust speed, seismic zone, snow drift, soil bearing. Below roughly 60 m this is the wrong product — for business jets, turboprops, helicopters and general aviation, the prefab aircraft hangar route ships as a containerised bolted kit for a fraction of the engineering. This page covers the heavy end.

The large aircraft hangar is a pre-engineered primary steel structure supplied as welded H-section columns and rafters with bolted site connections, paired with a space-truss or bolt-ball space-grid roof system. It is specified where the operation cannot tolerate an interior column: full wingtip clearance, unobstructed overhead crane coverage across the entire floor plate, and free positioning of tail stands, docks and maintenance platforms.

Six sub-systems make up the delivered structure. Understanding which is which matters when you compare two quotations, because suppliers omit different ones.
| Component | Configuration | Function |
| Primary frame | Welded H-section columns and rafters, Q355B, bolted site splices | Carries vertical and lateral load to the foundation; provides frame stiffness at the columns |
| Roof system | Space truss to ~110 m; bolt-ball or welded space grid above | Spreads roof load across the full span without intermediate columns; handles concentrated roof loads |
| Secondary steel | Purlins, girts, tie bars, sag rods, roof and wall bracing | Transfers cladding load to the primary frame and stabilises compression flanges |
| Crane system | Crane rails and monorail beams designed into the primary frame | Engine hoists, component removal, tail dock access — sized at design stage, retrofitted at a premium |
| Envelope | Insulated sandwich panel or single-skin profiled sheet with rooflights | Weather, thermal and fire performance; drives condensation behaviour |
| Door frame | Reinforced opening integrated into the primary structure | Resists and transmits the door’s reaction loads; we issue the load data, the leaves are procured locally |
| Parameter | Specification |
| Steel grade — primary | Q355B (ASTM A572 Gr 50 equivalent) |
| Steel grade — secondary | Q235B / Q355B cold-formed C and Z sections |
| Section form | Welded H-section, built up from plate; box section available for heavily loaded columns |
| Plate thickness range | 6–40 mm web, 8–60 mm flange |
| Clear span | 60–180 m, column-free |
| Clear height | 15 m upward |
| Crane capacity | 5–50 t, monorail or double-girder |
| Wind | Engineered to site gust speed; typhoon and cyclone regions to 250 km/h and above |
| Seismic | Engineered to site zone with ductile connection detailing |
| Snow | Up to 2.0 kN/m² with drift and unbalanced loading |
| Floor | Reinforced slab rated for aircraft jacking and engine hoists — designed by us, poured locally |
| Corrosion protection | Shot blast to Sa 2.5, hot-dip galvanizing 80–120 µm, or multi-coat epoxy system; chemical-resistant topcoat rated against aviation fuel and glycol de-icers |
| Fire rating — structure | Intumescent or fire-rated board to the rating your NFPA 409 group requires |
| Envelope core | Rock wool, PU or EPS sandwich panel; rock wool where fire rating governs |
| Design service life | 50 years structure |
| Design codes | EN 1990–1993 / AISC 360 + ASCE 7 + IBC / AS-NZS 1170 / GB 50017 + GB 50009 |
Full member schedules, connection details and calculation packages are issued per project. If you are preparing a tender, ask for the specification PDF before you write the enquiry — it will tell you which of these values are fixed and which are project-specific.

We engineer and document to the system your authority requires, and issue a stamped calculation package in the same system:
Where the project requires it, hangars are classified under NFPA 409 Groups I to IV by fire area and construction type, which sets the suppression requirement, and clearance is checked against the FAA AC 150/5300-13 Aircraft Design Group classification (Groups V and VI at this scale) or ICAO Annex 14 outside the US. We supply the structural side of that compliance — foam trench and drainage layout, sleeved penetrations, fire-rated panel options and the calculation pack your fire consultant needs. Suppression equipment is installed by licensed local contractors.
Certificates and test reports are listed on the certificates page.
Short summaries only — full scenario layouts, regional code guidance and aircraft-to-building sizing are on the application pages.
180 m column-free as a hybrid portal and space-truss system. Beyond roughly 100 m the roof is normally a full space grid rather than a truss, and the erection sequence has to be planned around temporary supports.
Yes, and it is the most common base-maintenance layout — typically a 70 to 90 m span for two B737 or A320 class bays, with the door split into two independent leaves.
We issue foundation and anchor bolt drawings as part of the structural package; your local contractor pours them. Order the drawings before you pour — a slab that misses the anchor layout is the most expensive error on this type of project.
Q355B primary steel (ASTM A572 Gr 50 equivalent), shot blasted to Sa 2.5 and hot-dip galvanized to 80–120 µm or given a multi-coat epoxy system, with a chemical-resistant topcoat rated against aviation fuel and glycol de-icers. Coastal and tropical sites get an upgraded specification.
Under NFPA 409 it depends on fire area and construction type. Most large commercial and military hangars land in a group that requires foam-water deluge. Your local authority has the final say and may apply its own standard.
Yes — EN 1990–1993 with EN 1090 execution class and CE marking, AISC 360 with ASCE 7 and IBC, AS/NZS 1170, or GB 50017 and GB 50009. Tell us which at enquiry stage; switching after design starts re-runs the calculations.
Members are numbered to match the erection drawings and packed by erection sequence. Standard members ship in 40 ft high-cube containers; spans above roughly 60 m generate out-of-gauge pieces that move as breakbulk or on flat rack. Send us the nearest port so we can price the overland leg, which often exceeds the ocean freight.
Both. We have installation teams working in 30+ countries, and we also supply as a bolted package with an engineer for supervision where local labour is more economical.
To return a budget figure in about two working days we need seven items: site location and nearest port; aircraft types and bay arrangement; required clear span, depth and eave height; door type and opening dimensions; wind speed, snow load, seismic zone and soil bearing capacity; crane capacity and hook height; and the design code and fire classification your authority requires.
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Canglong projects cover more than 120 countries and regions around the world, providing one-stop steel structure building solutions from design to installation.